Sounding rocket flight experiment for demonstrating “Furoshiki Satellite” for large phased array antenna

Abstract

University of Tokyo and Kobe University are planning a sounding rocket experiment of large membrane “Furoshiki Satellite” extension and large phased array RF transmission. The paper will describe the concept of “Furoshiki Satellite,” its application to solar power satellite, and the scenario of micro-gravity experiment using a small sounding rocket. University of Tokyo has been proposing the idea of “Furoshiki Satellite,” a large membrane or a net structure, say 1 km × 1 km in size, extended by satellites which hold its corners. The attitude and the shape of the membrane or net structure is controlled by these corner satellites. As one application of Furoshiki Satellite, a large solar power satellite can be configured by several solar cells and RF transmitters placed on several parts of the large net structure. It is difficult to control the position and attitude of the RF transmitters precisely, but using the “retro-directive” method, the tolerance of such position and attitude disturbance will be relaxed by large. This is one of promising systems’ concept of the future large solar power satellite or large antenna, because quite a large area can be obtained without any hard structure, and the weight will not depend very much on the size. To demonstrate the feasibility of the extension of large net structure and phased array performance, micro-gravity experiment is planned using a sounding rocket of JAXA/ISAS, Japan.